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GOE 534 AIRFOIL (goe534-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 534 AIRFOIL (goe534-il)
Reynolds number: 500,000
Max Cl/Cd: 93.24 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe534-il-500000.txt
Download as CSV file: xf-goe534-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 534 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.7196   0.06884   0.06558  -0.0608   1.0000   0.0356
 -13.750  -0.7762   0.05734   0.05387  -0.0700   1.0000   0.0354
 -13.500  -0.8099   0.04999   0.04637  -0.0757   1.0000   0.0354
 -13.250  -0.8407   0.04419   0.04047  -0.0794   1.0000   0.0353
 -13.000  -0.8652   0.03862   0.03478  -0.0838   1.0000   0.0353
 -12.750  -0.8671   0.03344   0.02938  -0.0900   1.0000   0.0355
 -12.500  -0.8577   0.03024   0.02596  -0.0930   1.0000   0.0357
 -12.250  -0.8461   0.02832   0.02386  -0.0934   1.0000   0.0359
 -12.000  -0.8367   0.02629   0.02173  -0.0927   1.0000   0.0363
 -11.750  -0.8232   0.02489   0.02029  -0.0917   1.0000   0.0368
 -11.500  -0.8076   0.02378   0.01916  -0.0907   1.0000   0.0373
 -11.250  -0.7915   0.02278   0.01811  -0.0895   1.0000   0.0378
 -11.000  -0.7754   0.02186   0.01713  -0.0882   1.0000   0.0382
 -10.750  -0.7394   0.02077   0.01593  -0.0906   0.9972   0.0389
 -10.500  -0.7006   0.01973   0.01477  -0.0934   0.9934   0.0395
 -10.250  -0.6641   0.01881   0.01372  -0.0954   0.9887   0.0401
 -10.000  -0.6278   0.01771   0.01258  -0.0976   0.9836   0.0409
  -9.750  -0.5907   0.01683   0.01168  -0.0998   0.9787   0.0418
  -9.500  -0.5562   0.01613   0.01095  -0.1011   0.9710   0.0429
  -9.250  -0.5191   0.01545   0.01020  -0.1029   0.9645   0.0440
  -9.000  -0.4831   0.01483   0.00949  -0.1044   0.9543   0.0450
  -8.750  -0.4469   0.01411   0.00877  -0.1060   0.9421   0.0465
  -8.500  -0.4083   0.01359   0.00821  -0.1079   0.9270   0.0482
  -8.250  -0.3716   0.01311   0.00764  -0.1093   0.9067   0.0503
  -8.000  -0.3393   0.01282   0.00729  -0.1098   0.8833   0.0528
  -7.750  -0.3106   0.01263   0.00699  -0.1094   0.8606   0.0562
  -7.500  -0.2827   0.01262   0.00689  -0.1089   0.8406   0.0601
  -7.250  -0.2549   0.01264   0.00684  -0.1083   0.8235   0.0644
  -7.000  -0.2270   0.01269   0.00677  -0.1077   0.8088   0.0692
  -6.750  -0.1993   0.01277   0.00680  -0.1071   0.7953   0.0727
  -6.500  -0.1713   0.01291   0.00674  -0.1066   0.7820   0.0761
  -6.250  -0.1448   0.01268   0.00653  -0.1060   0.7699   0.0790
  -6.000  -0.1174   0.01269   0.00645  -0.1054   0.7584   0.0818
  -5.750  -0.0897   0.01274   0.00637  -0.1048   0.7460   0.0841
  -5.500  -0.0637   0.01233   0.00594  -0.1042   0.7343   0.0866
  -5.250  -0.0368   0.01222   0.00578  -0.1036   0.7222   0.0889
  -5.000  -0.0094   0.01210   0.00561  -0.1030   0.7097   0.0910
  -4.750   0.0177   0.01201   0.00542  -0.1024   0.6967   0.0926
  -4.500   0.0448   0.01189   0.00521  -0.1018   0.6823   0.0942
  -4.250   0.0711   0.01150   0.00480  -0.1011   0.6671   0.0963
  -4.000   0.0979   0.01134   0.00459  -0.1005   0.6504   0.0980
  -3.750   0.1247   0.01123   0.00441  -0.0999   0.6319   0.1000
  -3.500   0.1515   0.01114   0.00422  -0.0992   0.6117   0.1016
  -3.250   0.1781   0.01109   0.00405  -0.0985   0.5906   0.1030
  -3.000   0.2049   0.01110   0.00393  -0.0978   0.5707   0.1042
  -2.750   0.2310   0.01089   0.00365  -0.0971   0.5539   0.1064
  -2.500   0.2576   0.01080   0.00350  -0.0965   0.5398   0.1087
  -2.250   0.2846   0.01077   0.00340  -0.0959   0.5271   0.1106
  -2.000   0.3120   0.01071   0.00330  -0.0954   0.5164   0.1122
  -1.500   0.3668   0.01066   0.00313  -0.0944   0.4967   0.1153
  -1.250   0.3938   0.01063   0.00304  -0.0938   0.4873   0.1179
  -1.000   0.4215   0.01055   0.00297  -0.0934   0.4792   0.1218
  -0.750   0.4489   0.01054   0.00293  -0.0929   0.4709   0.1269
  -0.500   0.4762   0.01047   0.00289  -0.0924   0.4632   0.1381
  -0.250   0.5033   0.01028   0.00287  -0.0920   0.4549   0.1862
   0.000   0.5298   0.01021   0.00292  -0.0914   0.4468   0.2465
   0.250   0.5575   0.01017   0.00297  -0.0910   0.4395   0.2801
   0.500   0.5846   0.01021   0.00304  -0.0905   0.4318   0.3034
   0.750   0.6120   0.01026   0.00311  -0.0901   0.4246   0.3226
   1.000   0.6394   0.01032   0.00317  -0.0896   0.4164   0.3397
   1.250   0.6661   0.01042   0.00326  -0.0890   0.4084   0.3565
   1.500   0.6937   0.01045   0.00334  -0.0886   0.4007   0.3740
   1.750   0.7203   0.01056   0.00344  -0.0880   0.3927   0.3895
   2.000   0.7476   0.01063   0.00353  -0.0876   0.3848   0.4046
   2.250   0.7743   0.01075   0.00362  -0.0870   0.3759   0.4185
   2.500   0.8010   0.01084   0.00373  -0.0865   0.3678   0.4321
   2.750   0.8275   0.01095   0.00383  -0.0859   0.3590   0.4448
   3.000   0.8540   0.01108   0.00395  -0.0854   0.3504   0.4595
   3.250   0.8801   0.01120   0.00408  -0.0848   0.3409   0.4734
   3.500   0.9061   0.01133   0.00421  -0.0842   0.3319   0.4871
   3.750   0.9318   0.01148   0.00435  -0.0835   0.3224   0.5021
   4.000   0.9575   0.01161   0.00450  -0.0828   0.3133   0.5202
   4.250   0.9823   0.01177   0.00467  -0.0821   0.3040   0.5398
   4.500   1.0076   0.01188   0.00484  -0.0814   0.2955   0.5639
   4.750   1.0313   0.01201   0.00503  -0.0805   0.2870   0.6027
   5.000   1.0783   0.01157   0.00529  -0.0844   0.2775   1.0000
   5.250   1.1027   0.01186   0.00550  -0.0837   0.2701   1.0000
   5.500   1.1277   0.01210   0.00571  -0.0829   0.2639   1.0000
   5.750   1.1524   0.01236   0.00593  -0.0822   0.2577   1.0000
   6.000   1.1754   0.01273   0.00621  -0.0812   0.2512   1.0000
   6.250   1.2007   0.01293   0.00642  -0.0806   0.2464   1.0000
   6.500   1.2247   0.01321   0.00667  -0.0798   0.2412   1.0000
   6.750   1.2471   0.01359   0.00699  -0.0787   0.2359   1.0000
   7.000   1.2713   0.01383   0.00725  -0.0779   0.2316   1.0000
   7.250   1.2950   0.01410   0.00751  -0.0771   0.2271   1.0000
   7.500   1.3171   0.01445   0.00783  -0.0760   0.2226   1.0000
   7.750   1.3386   0.01484   0.00819  -0.0749   0.2181   1.0000
   8.000   1.3622   0.01508   0.00846  -0.0740   0.2143   1.0000
   8.250   1.3842   0.01540   0.00878  -0.0730   0.2100   1.0000
   8.500   1.4040   0.01583   0.00916  -0.0716   0.2055   1.0000
   8.750   1.4249   0.01617   0.00953  -0.0704   0.2016   1.0000
   9.000   1.4467   0.01645   0.00984  -0.0694   0.1976   1.0000
   9.250   1.4661   0.01683   0.01021  -0.0680   0.1935   1.0000
   9.500   1.4821   0.01735   0.01068  -0.0661   0.1892   1.0000
   9.750   1.5006   0.01766   0.01105  -0.0645   0.1861   1.0000
  10.000   1.5182   0.01799   0.01143  -0.0628   0.1824   1.0000
  10.250   1.5332   0.01844   0.01187  -0.0608   0.1787   1.0000
  10.500   1.5448   0.01906   0.01246  -0.0584   0.1748   1.0000
  10.750   1.5615   0.01947   0.01293  -0.0568   0.1718   1.0000
  11.000   1.5774   0.01993   0.01344  -0.0551   0.1683   1.0000
  11.250   1.5905   0.02054   0.01406  -0.0532   0.1647   1.0000
  11.500   1.5998   0.02138   0.01488  -0.0510   0.1611   1.0000
  11.750   1.6144   0.02199   0.01556  -0.0495   0.1580   1.0000
  12.000   1.6278   0.02269   0.01631  -0.0480   0.1545   1.0000
  12.250   1.6381   0.02361   0.01724  -0.0464   0.1511   1.0000
  12.500   1.6439   0.02488   0.01850  -0.0446   0.1476   1.0000
  12.750   1.6569   0.02576   0.01947  -0.0435   0.1449   1.0000
  13.000   1.6675   0.02685   0.02062  -0.0423   0.1417   1.0000
  13.250   1.6749   0.02823   0.02203  -0.0412   0.1388   1.0000
  13.500   1.6781   0.03003   0.02383  -0.0400   0.1357   1.0000
  13.750   1.6866   0.03146   0.02535  -0.0392   0.1332   1.0000
  14.000   1.6946   0.03300   0.02696  -0.0384   0.1305   1.0000
  14.250   1.6993   0.03488   0.02889  -0.0378   0.1279   1.0000
  14.500   1.7000   0.03718   0.03121  -0.0371   0.1253   1.0000
  14.750   1.6991   0.03968   0.03376  -0.0366   0.1228   1.0000
  15.000   1.7046   0.04165   0.03583  -0.0363   0.1207   1.0000
  15.250   1.7064   0.04402   0.03828  -0.0360   0.1184   1.0000
  15.500   1.7051   0.04679   0.04110  -0.0359   0.1163   1.0000
  15.750   1.6989   0.05017   0.04451  -0.0360   0.1138   1.0000
  16.000   1.6944   0.05343   0.04784  -0.0362   0.1116   1.0000
  16.250   1.6949   0.05627   0.05078  -0.0365   0.1098   1.0000
  16.500   1.6927   0.05950   0.05410  -0.0370   0.1075   1.0000
  16.750   1.6867   0.06321   0.05787  -0.0376   0.1054   1.0000
  17.000   1.6783   0.06725   0.06194  -0.0384   0.1036   1.0000
  17.250   1.6709   0.07119   0.06593  -0.0391   0.1015   1.0000
  17.500   1.6676   0.07477   0.06962  -0.0400   0.0999   1.0000
  17.750   1.6625   0.07862   0.07357  -0.0409   0.0981   1.0000
  18.000   1.6563   0.08264   0.07766  -0.0420   0.0965   1.0000
  18.250   1.6489   0.08683   0.08189  -0.0432   0.0950   1.0000
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